CASIA OpenIR  > 综合信息系统研究中心
Design of Entry Trajectory Tracking Law for a Hypersonic Vehicle via Inversion Control
Zhiqiang Pu; Xiangmin Tan; Guoliang Fan; Jianqiang Yi
2012
Conference NameThe 10th World Congress On Intelligent Control and Automation
Source PublicationProceedings of the 10th World Congress On Intelligent Control and Automation
Conference DateJuly 6-8, 2012
Conference PlaceBeijing China
AbstractA nominal altitude-velocity longitudinal entry trajectory is planned and tracked for a Generic Hypersonic Vehicle (GHV) in this paper. The entry corridor is presented which is defined by the dynamic pressure, normal acceleration, heating constraints, and the so-called Quasi-Equilibrium Glide Condition (QEGC). The flyability of the vehicle along the nominal trajectory is carefully analyzed for further validation of the selected nominal trajectory. The control scheme mainly consists of two loops: a guidance loop and an attitude loop, of which the latter is separated into the slow and fast loops with the time-scale separation theory. Inversion control is employed in these three loops, and an integration feedback approach is especially added into the inversion controller to eliminate the tracking error. Simulations demonstrate that the nominal trajectory is designed appropriately and tracked well.
KeywordHypersonic Vehicle Entry Trajectory Tracking Inversion Control Integration Feedback
Indexed ByEI
Document Type会议论文
Identifierhttp://ir.ia.ac.cn/handle/173211/12359
Collection综合信息系统研究中心
Corresponding AuthorZhiqiang Pu
AffiliationInstitute of Automation, Chinese Academy of Sciences
Recommended Citation
GB/T 7714
Zhiqiang Pu,Xiangmin Tan,Guoliang Fan,et al. Design of Entry Trajectory Tracking Law for a Hypersonic Vehicle via Inversion Control[C],2012.
Files in This Item: Download All
File Name/Size DocType Version Access License
2012.WCICA-Design of(678KB)会议论文 开放获取CC BY-NC-SAView Download
Related Services
Recommend this item
Bookmark
Usage statistics
Export to Endnote
Google Scholar
Similar articles in Google Scholar
[Zhiqiang Pu]'s Articles
[Xiangmin Tan]'s Articles
[Guoliang Fan]'s Articles
Baidu academic
Similar articles in Baidu academic
[Zhiqiang Pu]'s Articles
[Xiangmin Tan]'s Articles
[Guoliang Fan]'s Articles
Bing Scholar
Similar articles in Bing Scholar
[Zhiqiang Pu]'s Articles
[Xiangmin Tan]'s Articles
[Guoliang Fan]'s Articles
Terms of Use
No data!
Social Bookmark/Share
File name: 2012.WCICA-Design of Entry Trajectory Tracking Law for a Hypersonic Vehicle via Inversion Control.pdf
Format: Adobe PDF
All comments (0)
No comment.
 

Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.